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      <dc:title>Numerical and experimental study of mode I delamination failure in composite laminates</dc:title>
      <dc:creator>Castillo-López, Germán</dc:creator>
      <dc:creator>Mesas, Álvaro</dc:creator>
      <dc:creator>García-Sánchez, Felipe</dc:creator>
      <dc:subject>Ingeniería estructural</dc:subject>
      <dc:description>Delamination is one of the most critical failure mechanisms in laminated composites. Usually it is&#xd;
assumed that delamination grows in a combination of modes I and II, but dominated by the mode I.&#xd;
In this work an experimental and numerical study of mode I delamination of laminated glass/epoxy&#xd;
[0/90]8S manufactured by resin infusion has been carried out. The value of has been obtained by&#xd;
the Double Cantilever Beam (DCB) test. Digital Image Correlation (DIC) has been used to measure the&#xd;
crack’s length.&#xd;
The numerical simulation was performed using two numerical techniques: Virtual Crack Closure&#xd;
Technique (VCCT) and the Cohesive Zone Model (CZM).&#xd;
Both techniques predict the onset of delamination. The VCCT is simple to use but it needs to define&#xd;
the area where delamination is going to start. The CZM allows the determination of the initial&#xd;
delamination area but it requires defining correctly the properties of the cohesive element.</dc:description>
      <dc:date>2015-07-21T09:36:15Z</dc:date>
      <dc:date>2015-07-21T09:36:15Z</dc:date>
      <dc:date>2015</dc:date>
      <dc:date>2015-07-21</dc:date>
      <dc:type>conference output</dc:type>
      <dc:identifier>http://hdl.handle.net/10630/10112</dc:identifier>
      <dc:identifier>http://orcid.org/0000-0002-8898-3376</dc:identifier>
      <dc:language>spa</dc:language>
      <dc:relation>3rd International Conference on mechanical models in structural engineering</dc:relation>
      <dc:relation>Sevilla</dc:relation>
      <dc:relation>Junio 2015</dc:relation>
      <dc:rights>open access</dc:rights>
      <dc:rights>by-nc-nd</dc:rights>
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